Airbus A310-300 vs. Cessna O-2 Skymaster

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Airbus A310-300 versus Cessna O-2 Skymaster
46.66 m 153 ft 1 in length 8.9 m 29 ft 2 in
15.8 m 51 ft 10 in height 2.87 m 9 ft 5 in
43.9 m 144 ft wingspan 11.58 m 38 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Two 210-hp Continental IO-360s
52,000 lb thrust per engine 210 hp
104,000 lb total thrust 420 hp
148,768 kg 328,000 lb MTOW 5,400 lb 2,449 kg
8,050 km 4,348 nm range 1,705 km 921 nm
482 knots 279 mph cruise speed 144 mph 232 km/h
190-230 passengers capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.